119 lines
3.5 KiB
Plaintext
119 lines
3.5 KiB
Plaintext
# ****************************************************************************
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# CUI
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#
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# The Advanced Framework for Simulation, Integration, and Modeling (AFSIM)
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#
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# The use, dissemination or disclosure of data in this file is subject to
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# limitation or restriction. See accompanying README and LICENSE for details.
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# ****************************************************************************
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# * * ************************************** * *
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# * ****** Demonstration input file ****** *
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# * ****** UNCLASSIFIED ****** *
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# * * ************************************** * *
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infrared_signature SIMPLE_INFRARED_SIGNATURE
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constant 1 watts/steradian
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end_infrared_signature
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optical_signature SIMPLE_OPTICAL_SIGNATURE
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constant 1 m^2
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end_optical_signature
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radar_signature SIMPLE_RADAR_SIGNATURE
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constant 1 m^2
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end_radar_signature
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aero GUESSED_AERO WSF_AERO
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// This is actually for an blue_sr_a2a_ir_missile, but we will assume similarity
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mach_and_cd 0.0 1.35 # ref AIAA 79-0091
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mach_and_cd 0.8 1.35 # ref AIAA 79-0091
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mach_and_cd 1.0 1.85 # ref AIAA 79-0091
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mach_and_cd 1.2 2.0 # ref AIAA 79-0091
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mach_and_cd 1.5 1.8 # ref AIAA 79-0091
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mach_and_cd 2.0 1.65 # ref AIAA 79-0091
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mach_and_cd 3.0 1.2 # ref AIAA 79-0091
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mach_and_cd 4.0 1.0 # ref AIAA 79-0091
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reference_area 0.02488 m2 # 17.8 cm dia (Wikipedia)
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cl_max 10.0 # Unknown
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aspect_ratio 17.7 # Unknown
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end_aero
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weapon_effects SIMPLE_EFFECT WSF_GRADUATED_LETHALITY
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radius_and_pk 100.0 m 0.75
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end_weapon_effects
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platform_type SIMPLE_MEDIUM_RANGE_MISSILE WSF_PLATFORM
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weapon_effects SIMPLE_EFFECT
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icon SA-10_Missile
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infrared_signature SIMPLE_INFRARED_SIGNATURE
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optical_signature SIMPLE_OPTICAL_SIGNATURE
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radar_signature SIMPLE_RADAR_SIGNATURE
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mover WSF_GUIDED_MOVER
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total_mass 161.5 kg # (Wikipedia)
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fuel_mass 55.0 kg
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# Isp values of 250 are typical of solid rocket motors of today
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specific_impulse 250.0 sec
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thrust 2500.0 lbf
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thrust_duration 12.12 sec
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update_interval 0.10 s
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aero GUESSED_AERO
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#show_status # Turns on some mass properties diagnostic output
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end_mover
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processor autopilot WSF_GUIDANCE_COMPUTER
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proportional_navigation_gain 30.0
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velocity_pursuit_gain 30.0
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g_bias 1.2
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maximum_commanded_g 40.0 g
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#omit_velocity_pursuit
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update_interval 0.1 s
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end_processor
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processor seeker WSF_PERFECT_TRACKER
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update_interval 0.10 s
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end_processor
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processor fuse WSF_AIR_TARGET_FUSE
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time_of_flight_to_arm 2.0 sec
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max_time_of_flight_to_detonate 140.0 sec
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detonate_on_mach_decreasing_to 1.0 # DRB Added 5/10/10
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detonate_below_height_AGL 0.0 ft # -200.0 m
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# DRB: Make sure does not detonate prematurely during generation.
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# PROBLEM: For sea level test, cannot set negative!
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end_processor
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end_platform_type
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weapon_effects SIMPLE_EFFECT WSF_GRADUATED_LETHALITY
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# A Pk of 1.0 is needed for weapon launch computer generation.
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radius_and_pk 100.0 m 1.0
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end_weapon_effects
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weapon SIMPLE_MEDIUM_RANGE_MISSILE WSF_EXPLICIT_WEAPON
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launched_platform_type SIMPLE_MEDIUM_RANGE_MISSILE
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weapon_effects SIMPLE_EFFECT
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quantity 4
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firing_delay 0.5 sec
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salvo_interval 5.0 sec
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slew_mode azimuth_and_elevation
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azimuth_slew_limits -180.0 deg 180.0 deg
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elevation_slew_limits 10.0 deg 70.0 deg
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end_weapon
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